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Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds [microform] / John E. Lamar ... [et al.] (NASA/TP ; 2001-210629)

Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds [microform] / John E. Lamar ... [et al.] (NASA/TP ; 2001-210629)
Microform図書
2001<YCA-NAS 1.60:210629>
National Diet Library
  • Subject Heading...d tunnel tests Wing profiles Geometry Flight tests Data i...

Water tunnel flow visualization study through poststall of 12 novel planform shapes [microform] / Gregory M. Gatlin, Dan H. Neuhart (NASA technical memorandum ; 4663)

Water tunnel flow visualization study through poststall of 12 novel planform shapes [microform] / Gregory M. Gatlin, Dan H. Neuhart (NASA technical memorandum ; 4663)
Microform図書
1996<YCA-NAS 1.15:4663>
National Diet Library
  • Subject Heading...flow Planforms Wing profiles Aerodynamic configurations

遷音速風洞フラッタ緊急停止装置性能試験　その1:半截模型カート用装置の効果

遷音速風洞フラッタ緊急停止装置性能試験　その1:半截模型カート用装置の効果
Digital文書・図像類
鈴木, 弘一, 細江, 信幸, 飯島, 由美, 小松, 行夫, 国益, 徹也, 安藤, 泰勝, 半沢, 麻雄, 鈴木, 誠三, Suzuki, Koichi, Hosoe, Nobuyuki, Iijima, Yoshimi, Komatsu, Yukio, Kunimasu, Tetsuya, Ando, Yasukatsu, Hanzawa, Asao, Suzuki, Seizo航空宇宙技術研究所1994-11航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory668p.1-17
Other Libraries in Japan
  • Subject Heading...trol gust load wing profile turntable pneumatic cylinder ...

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